# Boeing 767-3G5 - Type: Aircraft model (FAA registry) - Registry code: 1385126 - Manufacturer (registry): BOEING - Model: 767-3G5 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 351 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-767-3g5 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB WPR11LA071](https://openairdocs.org/ntsb/WPR11LA071), Dec 3, 2010: Boeing 767 (N584HA), Pago Pago, Antarctica, no damage. Probable cause: The airplane’s encounter with convectively-induced turbulence, which resulted in serious injury to one flight attendant. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20101203053579A](https://openairdocs.org/incident/20101203053579A), Dec 3, 2010: Boeing 767-3G5 (N584HA), Honolulu, HI, No damage. Aircraft climbing through flight level 180 encountered clear air turbulence resulting in 2 flight attendant injuries, one minor (facial contusions) and one… ## Service difficulty reports (724, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR HALA2013091000105](https://openairdocs.org/sdr/HALA2013091000105), Sep 10, 2013: DRIVE ASSY. FAILED. BOTH WEATHER RADARS INOPERATIVE. REPLACED WX RADAR ANTENNA DRIVE. OPS CHECK OK BOTH WX RADAR SYSTEMS IAW M/M34-43--05. - [SDR HALA2013072400093](https://openairdocs.org/sdr/HALA2013072400093), Jul 24, 2013: TRU. FAULTED. VERIFICATION FLIGHT FOR APU COMPLETED UNSATISFACTORY, FAILED. EICAS APU FAULT. TROUBLESHOT IAW FIM 49-11-00-101, R & R TRU IAW 24-32-04-404-003 APU STARTED NORM - [SDR HALA2013062200083](https://openairdocs.org/sdr/HALA2013062200083), Jun 22, 2013: COUPLING. FAILED. BOTH HF RADIOS NOT CHANNELIZING. R & R LT AND RT HF ANTENNA COUPLERS IAW AMM TASK 23-11-01-024-001/23-11-01-424-008, R & R LT HF TRANSCEIVER IAW AMM TASK 23-11- - [SDR HALA201306240135](https://openairdocs.org/sdr/HALA201306240135), Jun 22, 2013: COUPLER. FAILED. BOTH HF RADIOS NOT CHANNELIZING. R & R LT AND RT HF ANTENNA COUPLERS IAW AMM TASK 23-11-01-024-001/23-11-01-424-008, R & R LT HF TRANSCEIVER IAW AMM TASK 23-11- - [SDR HALA2013060500075](https://openairdocs.org/sdr/HALA2013060500075), Jun 5, 2013: CIRCUIT CARD. MALFUNCTIONED. EICAS MESSAGE, FOUND RT ENG FIRE LOOP 1. REPLACED CIRCUIT CARD M683, RT WING FIRE LOOP 1, FIRE DETECT CONTROL CARD IAW AMM 26-10-01. OPS CHECKED GOOD. OK FOR SE - [SDR HALA2013042900049](https://openairdocs.org/sdr/HALA2013042900049), Apr 29, 2013: STARTER. FAULTED. APU FAULT DISPLAYED WHEN APU START ATTEMPTED ON FINAL APPROACH. BITE CHECKED ECU BOX. FAULTED APU STARTER. REPLACED APU STARTER IAW AMM 49-41-01. SECURITY AND C - [SDR HALA2013040200033](https://openairdocs.org/sdr/HALA2013040200033), Apr 2, 2013: INTERROGATOR. MALFUNCTIONED. LT WING SLIDE ILLUMINATED DURING TAKE OFF ROLL, 100 KNOTS. R & R OVERWING ESCAPE SLIDE INTERROGATOR IAW AMM 25-65-12, OPS CHECKED GOOD. - [SDR HALA2013040100032](https://openairdocs.org/sdr/HALA2013040100032), Apr 1, 2013: INTERROGATOR. FAILED. LEFT WING EXIT SLIDE ILLUMINATED DURING TAKE OFF ROLL. R & R WING ESCAPE SLIDE INTEROGATOR IAW AMM 25-65-12, OPS CHECK GOOD. - [SDR HALA2013021300020](https://openairdocs.org/sdr/HALA2013021300020), Feb 13, 2013: ENGINE. MALFUNCTIONED. RT ENGINE EPR, N1, N2, F/F ALL FLUCTUATE. CLIMB EPR 1.5 PERCENT, N1 .5 PERCENT, N2 .2 PERCENT, F/F 200LBS LESS IN CRUISE. - [SDR HALA2013021300019](https://openairdocs.org/sdr/HALA2013021300019), Feb 13, 2013: SLIDE. DETACHED. DOOR SLIDE FOUND R4 DETACHED FROM DOOR AFTER CATERERS ATTEMPTED ENTRY (BLOCKED SEATS ROWS 36-45). (MAIN ENTRY DOOR SLIDES PASSSENGER CONFIG). INSTALLED R4 SLIDE - [SDR HALA2013021200018](https://openairdocs.org/sdr/HALA2013021200018), Feb 12, 2013: CONNECTOR. BROKEN. AT DEPARTURE TIME CREW REPORTS MID GALLEY EMERGENCY LIGHTING FLOOR STRIP LT SIDE CONNECTOR BROKE LOOSE. RESECURED MID GALLEY EMERGENCY LIGHT FLOOR STRIP WIRES. - [SDR HALA2013013100014](https://openairdocs.org/sdr/HALA2013013100014), Jan 31, 2013: CONNECTOR. DIRTY. AIR TURNBACK, APU AUTO SHUTDOWN, APU VERIFICATION UNSATISFACTORY. ECU BIT INDICATES "HIGH TEMP" WITH MINI FLAGS 11, 45 & 48. PERFORMED MEGGER TEST FOUND NR 2 TH - [SDR HALA2013011300011](https://openairdocs.org/sdr/HALA2013011300011), Jan 13, 2013: STARTER. FAILED. AFTER PUSH BACK, AFTER CONTROL SWITCH TO RUN N2 DECREASED TO 23 PERCENT, ESS, & CAS RAMP CONTROL REPORTED FIRE/SPARKS COMING FROM LT ENGINE. FUEL CONTROL SWITCH - [SDR HALA2013011100009](https://openairdocs.org/sdr/HALA2013011100009), Jan 11, 2013: BATTERY. INOPERATIVE. APU UNABLE TO START COMPLETELY. R & R APU BATTERY IAW AMM 24-31-04. OPERATION CHECK GOOD. OK FOR SERVICE. - [SDR HALA2013010200001](https://openairdocs.org/sdr/HALA2013010200001), Jan 2, 2013: WARNING MESSAGE. ILLUMINATED. AFTER RT ENGINE START HPSOV ILLUMINATED ON EICAS AND STATUS PAGE. RESET THE EICAS IAW FIM 31-41, FAULT TREE 812. CHECKED AIR BITE AMM 36-11-00-715-149. RAN ENG. - [SDR HALA2012123100237](https://openairdocs.org/sdr/HALA2012123100237), Dec 31, 2012: WARNING LIGHT. FALSE ACTIVATION. RT ENGINE HPSOV ON EICAS AFTER ENGINE START. RESET EICAS IAW FIM 31-41- FAULT 2 TREE 812, CHECKED AIR BITE SYS, NO PR'S NOTED. RAN ENG. OPS CHECKED GOOD IAW AMM - [SDR HALA2012120300230](https://openairdocs.org/sdr/HALA2012120300230), Dec 3, 2012: EEC. MALFUNCTIONED. LEFT ENGINE EEC C1 LT ENG CONTROL. R & R NR 1 ENGINE EEC IAW AMM 73-21-04. RUN/OPS CHECK PENDING AND (STEPS G) 5-8 PENDING. ACCOMPLISHED STEPS 5-8 & RUN. CONDIT - [SDR HALA2012102900224](https://openairdocs.org/sdr/HALA2012102900224), Oct 29, 2012: CONNECTOR. SHORTED. F/A REPORTED STRONG ELECTRICAL ODOR NEAR 4R DOOR. COLLARED CIRCUIT B H006 AND DISCONNECTED CONNECTOR PLUG FROM WATER AIR COMPRESSOR. (POTABLE WATER SYS). - [SDR HALA2012101900221](https://openairdocs.org/sdr/HALA2012101900221), Oct 19, 2012: PROCESSOR. FAULTY. B1 FAULT FOUND ON FQIS PROCESSOR.. BITE IAW FIM 28-41 TASK 852. B1 FAULT-FIM 28-41 TASK 856. IAW FIM REPLACED FQIS PROCESSOR IAW AMM 28-41-08. OPS CHECK GOOD. - [SDR HALA2012091700211](https://openairdocs.org/sdr/HALA2012091700211), Sep 17, 2012: LINE. LEAKING. RIGHT HYD QTY (EICAS), PERFORMED QRH RT WAS .48 RF WHEN HYD QTY EICAS CAME ON. CENTER HYD QUANITY .55 RF AT SHUTDOWN INFLT .93 TO .78 TO .74 RF. NEW HYD FLEX-LI - [SDR HALA2012091700208](https://openairdocs.org/sdr/HALA2012091700208), Sep 17, 2012: WARNING LIGHT. FALSE ACTIVATION. NR 1 ENGINE AND APU FIRE LOOP SHOWED EICAS MESSAGE NO TEST. PERFORMED ENG AND APU FIRE LOOP TEST IAW FIM 26-15 FIG 803 & 804. OPS CHECKED GOOD, NO FAULTS NOTED. - [SDR HALA2012090900204](https://openairdocs.org/sdr/HALA2012090900204), Sep 9, 2012: WARNING LIGHT. FALSE ACTIVATION. DURING CLIMB OUT AND DESCENT EICAS MESSAGE "AILERON LOCKOUT. "ACCOMPLISHED FIM 27-11 FAULT TREE. NO DEFECTS NOTED. OK FOR SERVICE. - [SDR HALA2012090700203](https://openairdocs.org/sdr/HALA2012090700203), Sep 7, 2012: WARNING MESSAGE. ILLUMINATED. DURING CLIMB AT APPROX 290 KTS RECEIVED AN AILERON LOCKOUT EICAS AND AILERON LOCK LIGHT. AFTER 10 MINS MESSAGE CLEARED. OPS NORMAL. PERFORMED FIM PROCEDURE 27-1 - [SDR HALA2012090400201](https://openairdocs.org/sdr/HALA2012090400201), Sep 4, 2012: WARNING MESSAGE. FALSE ACTIVATION. EICAS MESSAGE, LT ENG CONTROL DISPLAYED ALONG WITH STATUS MESSAGE, LT ENG CONTROL AND LT ENG EEC C1. RAN LT ENG BITE CK LT PIMU. FOUND FAULTS EEC CHANNEL B SVA - [SDR HALA2012090400199](https://openairdocs.org/sdr/HALA2012090400199), Sep 4, 2012: FMU. MALFUNCTIONED. DURING ENGINE START ENG VALVE ADVISORY LIGHT REMAINED ON DURING START. AFTER ENGINE STARTED OK. AT IDLE LIGHT AND LT ENG VALVE EICAS LIGHT WENT OUT. R & R LEFT - [SDR HALA2012082000195](https://openairdocs.org/sdr/HALA2012082000195), Aug 20, 2012: COUPLER. FAULTED. TRANSMISSION AND RECEPTION ON RT-HF INOPERATIVE. (IT WOULD NOT CHANELIZE). FOUND RT TRANCEIVER FAULTING HF COUPLER. R & R NR 2 HF COUPLER IAW MM 23-11-01. GROUN - [SDR HALA2012082000194](https://openairdocs.org/sdr/HALA2012082000194), Aug 20, 2012: RADIO. MALFUNCTIONED. TRANSMISSION AND RECEPTION ON LT-HF INOPERATIVE (IT WOULD NOT CHANELIZE. RERACKED NR 1 HF TRANSCEIVER IAW MM 23-11-03. GROUND CHECK OK. - [SDR HALA2012081800192](https://openairdocs.org/sdr/HALA2012081800192), Aug 18, 2012: APU. AUTO SHUTDOWN. APU AUTO SHUTDOWN IN FLIGHT. EICAS MESSAGE, APU FAULT. R & R APU IAW M266-767. LEAK AND OPS CHECKED OK. - [SDR HALA2012073100188](https://openairdocs.org/sdr/HALA2012073100188), Jul 31, 2012: PUMP. LEAKING. FOUND NR 1 ENG HYD PUMP LEAKING. R & R NR 1 HYD EDP IAW AMM 29-11-05, LEAK & OPS CHECKED OK. - [SDR HALA2012071900177](https://openairdocs.org/sdr/HALA2012071900177), Jul 19, 2012: COMPENSATOR. FAULTY. RT FUEL QUANITY INDICATOR AND BOTH TOTALIZERS WENT BLANK. 40 MIN LATER RT QUANTITY GAUGE WENT FROM 31.7 DOWN TO 29.2 OSCILATING THERE FOR ABOUT 10 MINS. PERFORM - [SDR HALA2012071800176](https://openairdocs.org/sdr/HALA2012071800176), Jul 18, 2012: RELIEF VALVE. LEAKING. RIGHT FUEL TANK QUANTITY DECREASED 1500 LBS DURING CLIMB WHILE BOTH CENTER TANK PUMPS ARE ON AND OPERATING. FOUND PRESSURE RELIEF VALVE LEAKING. REPLACED PRESSU - [SDR HALA2012071000170](https://openairdocs.org/sdr/HALA2012071000170), Jul 10, 2012: BYPASS VALVE. LEAKING. APU AUTO SHUTDOWN AT GATE. BITE APU IAW FIM HIGH OIL TEMP FAULT IAW FIM 49-11-00, FIG 110. NO OTHER FAULTS FOUND. IAW FIM REPLACED OIL COOLER BYPASS VALVE IAW A - [SDR HALA2012070200165](https://openairdocs.org/sdr/HALA2012070200165), Jul 2, 2012: COUPLING. SHEARED. RT ENGINE STARTER TO GEARBOX COUPLING SHEARED. R & R STARTER DRIVE COUPLING IAW AMM 72-61-09. - [SDR HALA2012062900163](https://openairdocs.org/sdr/HALA2012062900163), Jun 29, 2012: MODULE. MALFUNCTIONED. FIRE BELL WARNING AT 95 KTS ON TAKEOFF. ABORT EXERCISED. COULD NOT CANCEL/MUTE BELL CHIME AND NO VISUAL INDICATION NOTED. INSPECTED WIRING AT CONNECTOR D4349P & - [SDR HALA2012060500159](https://openairdocs.org/sdr/HALA2012060500159), Jun 5, 2012: WARNING LIGHT. FALSE ACTIVATION. RT ENG BLEED OFF EICAS AND LIGHT APPEARED TWICE DURING FLIGHT. FIRST DURING CLIMB FOR 30 SECONDS, SECOND DURING CRUISE DESCENT FOR 10-15 SECONDS. RAN NR NR 2 EN - [SDR HALA2012053100153](https://openairdocs.org/sdr/HALA2012053100153), May 31, 2012: FMC. MALFUNCTIONED. AFTER LANDING LT FMC INOPERATIVE. TROUBLESHOT IAW FIM 34-61-00/101 FIG 111. MESSAGE CLEARED, NO FAULTS AT THIS TIME. - [SDR HALA2012050900134](https://openairdocs.org/sdr/HALA2012050900134), May 9, 2012: BLADE. DAMAGED. ON WALKAROUND FOUND RT ENGINE NR 6 FAN BLADE HAS FOD DAMAGE, APPROXIMATELY TWELVE INCHES FROM BLADE ROOT (AREA F). BLENDED DAMAGED AREA WITHIN LIMITS IAW AMM 72 - [SDR HALA2012042900127](https://openairdocs.org/sdr/HALA2012042900127), Apr 29, 2012: SENSOR. OPEN. CLIMBING THROUGH 9,000' RECEIVED "RT FWD WINDOW" LIGHT AND INOPERATIVE LIGHT ON, FOLLOWED QRH. LIGHT STAYED ON, RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-41-00 - [SDR HALA2012042900126](https://openairdocs.org/sdr/HALA2012042900126), Apr 29, 2012: CONTROL UNIT. MALFUNCTIONED. CLIMBING THROUGH APPROX 25,000' RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. RET - [SDR HALA2012021800126](https://openairdocs.org/sdr/HALA2012021800126), Apr 29, 2012: CONTROL UNIT. MALFUNCTIONED. CLIMBING THROUGH APPROX 25,000', RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. AC - [SDR HALA2012041400125](https://openairdocs.org/sdr/HALA2012041400125), Apr 14, 2012: GEARBOX. BINDING. NR 3 SLAT E/B GEARBOX BINDING IN RETRACT POSITION. R & R NR 3 SLAT INBD GEARBOX IAW AMM 27-81-20. INSPECTED AND IS SAFE FOR THE INTENDED FLIGHT. - [SDR HALA2012031800113](https://openairdocs.org/sdr/HALA2012031800113), Mar 18, 2012: CONNECTOR. UNSECURE. ON OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING BETWEEN L1 & R1 DOOR INOPERATIVE. RECONNECTED AND RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR. OPS CHECKE - [SDR HALA2012030500099](https://openairdocs.org/sdr/HALA2012030500099), Mar 5, 2012: WARNING LIGHT. MULTIPLE FAIL. IN CRUISE, NO LAND 3 INDICATED ON THE ASA INDICATOR. RA WARNING INDICATED BRIEFLY ON CAPT ADI. FLT FAULTS INDICATED CRA NO LAND 3. ON FLT LOGS 1 AND 2 PERFORMED - [SDR HALA2012022900088](https://openairdocs.org/sdr/HALA2012022900088), Feb 29, 2012: WARNING LIGHT. FALSE ACTIVATION. FLT DECK TEMP DISPLAYED AND FLT COMPT TEMP "INOPERATIVE" LIGHT ILLUMINATED IN "AUTO", MANUAL OPS NORMAL. PERFROMED BITE TEST ON ZONE TEMP & PACK CONTROLLERS, NO - [SDR HALA2012022600081](https://openairdocs.org/sdr/HALA2012022600081), Feb 26, 2012: WARNING MESSAGE. FALSE ACTIVATION. LEFT PACK TEMPERATURE EICAS MESSAGE. LT PACK INOP ON OVERHEAD MULTIPLE TIMES AT 5 SECS EACH TIME, SELECTED STANDBY IAW QRH. BITE CHECKED LT PACK CONTROLLER, NO - [SDR HALA2012021800064](https://openairdocs.org/sdr/HALA2012021800064), Feb 18, 2012: WIRE. DAMAGED. RIGHT IDG TEMPERATURE SENSOR DISPLAYED IDG OUT: 80-180 IDG RISE 8-180 AT TOP OF CLIMB. ACCOMPLISHED FIM 24-20-00, REPAIRED DAMAGED WIRE, JACKED ON D10966 PLUG, - [SDR HALA201202180006](https://openairdocs.org/sdr/HALA201202180006), Feb 18, 2012: WARNING LIGHT. ILLUMINATED. APU DISPLAYED "APU FAULT" AND APU AUTO SHUTDOWN DURING VERIFICATION FLIGHT, VERIFICATION FAILED. BITE CHECKED ECU, FOUND "AUTO SHUTDOWN GEN FILTER" ACCOMPLISHED - [SDR HALA2012021800063](https://openairdocs.org/sdr/HALA2012021800063), Feb 18, 2012: APU. FAULTED. APU DISPLAYED "APU FAULT" AND APU AUTO SHUTDOWN DURING A VERIFICATION FLIGHT. BITE CHECKED ECU, FOUND "AUTO SHUTDOWN GENERATOR FILTER" ACCOMPLISHED FIM 49-11-00 - [SDR HALA2012021200056](https://openairdocs.org/sdr/HALA2012021200056), Feb 12, 2012: COMPUTER. MALFUNCTIONED. DURING FLT, BOTH FMC`S BLANKED OUT. THEN DISPLAYED "RESET TIMEOUT". RESELECTED FMC AND DISPLAYED NORMALLY EXCEPT ON PROGRAM PAGE 2, LT & RT FUEL USED AND TOTAL - [SDR HALA2012021200055](https://openairdocs.org/sdr/HALA2012021200055), Feb 12, 2012: WARNING MESSAGE. ILLUMINATED. RECEIVED AN EICAS MESSAGE OF RT PACK TEMPERATURE. RT SELECTOR PLACED IN STBY-N-OPS NORMAL. PERFORMED BITE TEST IAW FIM 21-51-00, FIG 103. MESSAGE NOT ACTIVE. OK All 724: https://openairdocs.org/model/boeing-767-3g5/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.